摘要
本文用气动检测法,对航空发动机叶片叶型进行无损检测,对发动机基元叶型生成技术、三维叶片优化设计方法,表面气流参数分布准则及气动性能与型面几何形状匹配,数值模拟方式及叶型研究和分析的方法进行测试,验证了方法的有效性,完善了叶片设计方法,创新了叶片叶型检测的理论与实践。
The paper applies aerodynamic detection method to detect aero-engine nondestructively. In this paper, generating technologyofelementaryblade, optimization design of 3D blade, airflow parameter distribution criteria of blade surface, alignment between aero performance and blade geometry, numerical simulation method and method of blade research and analysis are tested. The paper validates the methods, improves the blade design and innovates the theory and practice of blade profile testing.
出处
《长春理工大学学报(自然科学版)》
2007年第3期60-62,共3页
Journal of Changchun University of Science and Technology(Natural Science Edition)
关键词
航空发动机
叶片叶型
无损检测
气动试验
Aero-engine
blade profile
nondestructive detection
aerodynamic examination